Research Article
A New Adaptive Federated Cubature Kalman Filter Based on Chi-Square Test for SINS/GNSS/SRS/CNS Integration
Table 1
Parameters in simulations.
| Initial position | East longitude | 108.9° | North latitude | 34.025° | Altitude | 40 km |
| Initial velocity | East | 151 m/s | North | 125 m/s | Up | 125 m/s |
| Initial attitude | Pitch | 0° | Roll | 0° | Yaw | 0° |
| Gyro parameters | Constant drift | 0.5°/h | White noise | 0.5°/h | Sampling frequency | 10 Hz |
| Accelerometer parameters | Zero bias | 0.1 mg | White noise | 0.1 mg | Sampling frequency | 10 Hz |
| GNSS parameters | Pseudorange measurement error | 20 m | Pseudorange rate measurement error | 0.5 m/s | Sampling frequency | 10 Hz |
| SRS parameters | Redshift measurement error | 10^-8 | Sampling frequency | 1Hz |
| CNS parameters | Measurement error | 15m | Sampling frequency | 1Hz |
| Barometric altimeter parameter | Altitude measurement error | 10m | Sampling frequency | 1Hz |
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